WO2018066257A1 - 接着剤組成物およびこれを含有する接着剤層、支持接合体、およびこの支持接合体を備えるガスバリア性評価装置 - Google Patents
接着剤組成物およびこれを含有する接着剤層、支持接合体、およびこの支持接合体を備えるガスバリア性評価装置 Download PDFInfo
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- WO2018066257A1 WO2018066257A1 PCT/JP2017/030365 JP2017030365W WO2018066257A1 WO 2018066257 A1 WO2018066257 A1 WO 2018066257A1 JP 2017030365 W JP2017030365 W JP 2017030365W WO 2018066257 A1 WO2018066257 A1 WO 2018066257A1
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- adhesive composition
- adhesive
- gas barrier
- barrier property
- epoxy resin
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J163/00—Adhesives based on epoxy resins; Adhesives based on derivatives of epoxy resins
- C09J163/04—Epoxynovolacs
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J11/00—Features of adhesives not provided for in group C09J9/00, e.g. additives
- C09J11/02—Non-macromolecular additives
- C09J11/06—Non-macromolecular additives organic
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09J—ADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
- C09J7/00—Adhesives in the form of films or foils
- C09J7/20—Adhesives in the form of films or foils characterised by their carriers
Definitions
- the present invention relates to an adhesive composition, an adhesive layer containing the same, a support bonded body, and a gas barrier property evaluation apparatus including the support bonded body.
- FIG. 3 is a schematic diagram schematically showing a configuration of a gas barrier property evaluation apparatus using a differential pressure method, which is shown as a reference example.
- FIG. 4 is a schematic diagram schematically showing a configuration of a gas barrier property evaluation apparatus using an isobaric method shown as a reference example.
- the gas barrier property evaluation apparatus 30 using the differential pressure method includes a tank 31, a sample chamber 32, a detector 33, and a vacuum pump.
- a film 321 to be measured is supported by a support body 322 provided on the base material 323.
- the vacuum pump 34 is operated to generate a differential pressure in the sample chamber 32. Specifically, gas is introduced at an arbitrary pressure from the tank 31 side through the film 321 in the sample chamber 32, and the vacuum pump 34 side is brought into an ultrahigh vacuum state. Then, water or gas is allowed to flow out of the tank 31, and the amount of water or gas that passes through the film 321 is detected by the detector 33.
- the gas barrier property evaluation apparatus 40 using the isobaric method includes a tank 41, a sample chamber 42, and a detector 43.
- a film 421 to be measured is supported by a support body 422 provided on the base material 423.
- the sample chamber 42 is kept at normal pressure, and water or gas is allowed to flow out of the tank 41, and the amount of water or gas that passes through the film 421 is detected by the detector 43. Detect with.
- the film is not damaged unlike the gas barrier property evaluation apparatus 30 (see FIG. 3) using the differential pressure method.
- the gas barrier property evaluation device 40 has a problem that it takes a longer time for measurement and evaluation than the gas barrier property evaluation device 30.
- the gas barrier property evaluation apparatuses shown in Patent Documents 1 and 2 are disclosed. All of these gas barrier property evaluation apparatuses are configured to fix the base material and the support in the sample chamber using an adhesive, and examples of the adhesive used at that time include beeswax. Yes.
- the temperature in the sample chamber may be raised to, for example, about 80 ° C. to 130 ° C. to remove moisture in the sample chamber. Therefore, the adhesive used for the gas barrier property evaluation apparatus is required to have heat resistance and heat cycle resistance. However, when beeswax is used as an adhesive, it cannot be said that heat resistance is sufficient.
- a commonly used thermoplastic adhesive such as polyester (such as PET and PA), acrylic adhesive, and / or cyanoacrylate adhesive is used as the adhesive.
- a phenol novolac type epoxy compound Patent Document 3
- a hydrogenated phenol novolac type epoxy resin Patent Document 4
- a cationic polymerization initiator used for electronic parts may also be used as an adhesive in a gas barrier property evaluation apparatus. Conceivable.
- a polyester-based thermoplastic adhesive has poor coatability and must be bonded under high temperature conditions, which may cause damage to the support.
- Acrylic adhesives are also insufficient in terms of heat resistance and adhesiveness.
- a cyanoacrylate-based adhesive it is difficult to handle because there are many outgasses and a drying time after bonding is also required.
- the phenol novolac type epoxy resin disclosed in Patent Document 3 is used as an adhesive, the support that can be used in the sample chamber is limited from the viewpoint of adhesiveness.
- the amount of water or gas measured by the gas barrier property evaluation apparatus is very small, and these are easily affected by the outgas generated from the adhesive. Therefore, it is necessary to use a low outgas adhesive particularly for the gas barrier property evaluation apparatus.
- the present invention has been made in view of the above-mentioned problems, and its purpose is excellent in heat resistance and heat cycle resistance, is easy to handle, and contributes to low outgas, so it is also suitable for a gas barrier property evaluation apparatus. It is in providing the adhesive composition used for this.
- the inventors of the present invention have been diligently studying an adhesive composition that can be suitably used in a gas barrier property evaluation apparatus. By combining a specific novolac type epoxy resin and a thermal cation type polymerization initiator in combination. The present inventors have found that the above problems can be solved, and have completed the present invention.
- an adhesive composition according to an embodiment of the present invention contains a novolac type epoxy resin represented by the following formula (1) and a thermal cationic polymerization initiator represented by the following formula (2). It is.
- n represents an integer of 0 to 10.
- R 1 represents any one of the following groups.
- R 2 represents any of the following groups.
- Y is BF 4 ⁇ , PF 6 ⁇ , SbF 6 ⁇ , or (BX 4 ) ⁇ (wherein X is substituted with at least two fluorine or trifluoromethyl groups.
- An adhesive composition according to an embodiment of the present invention includes, as a novolak type epoxy resin, a phenol novolak type epoxy resin, a xylene novolak type epoxy resin, a dicyclopentadiene (DCPD) phenol novolak type epoxy resin, and a biphenyl novolak type epoxy resin. It is preferable to contain 1 type (s) or 2 or more types selected from the group which consists of.
- the adhesive composition according to an embodiment of the present invention includes 90 to 99.5 parts by weight of the novolac type epoxy resin and 100 parts by weight of the thermal cationic polymerization initiator with respect to 100 parts by weight of the adhesive composition. It is preferable to contain 5 to 10 parts by weight.
- One embodiment of the present invention also provides an adhesive for a gas barrier property evaluation apparatus containing the adhesive composition.
- One embodiment of the present invention further provides an adhesive layer containing the adhesive composition.
- One embodiment of the present invention further provides a support joined body including a base material, an adhesive layer laminated on the base material, and a support laminated on the adhesive layer.
- the adhesive layer in the support bonded body is an adhesive layer according to an embodiment of the present invention.
- One embodiment of the present invention further provides a gas barrier property evaluation apparatus including the support assembly according to one embodiment of the present invention.
- the present invention it is excellent in heat resistance, heat cycle resistance and adhesiveness, and contributes to low outgas. Therefore, it is possible to provide an adhesive composition that can be suitably used for a gas barrier property evaluation apparatus.
- the adhesive composition according to this embodiment (hereinafter, also simply referred to as “adhesive composition”) contains a novolac type epoxy resin and a thermal cationic polymerization initiator.
- the novolac type epoxy resin used in this embodiment is represented by the following formula (1).
- n represents an integer of 0 to 10, and n is preferably an integer of 0 to 5.
- R 1 represents any one of the following groups.
- R 1 is preferably a hydrogen atom.
- R 2 represents any of the following groups.
- R 2 is preferably a methylene group.
- the novolak type epoxy resin include a phenol novolak type epoxy resin, a xylene novolak type epoxy resin, a dicyclopentadiene (DCPD) phenol novolak type epoxy resin, a biphenyl novolak type epoxy resin, and the adhesive composition. It is preferable to contain one or more selected from these resins.
- particularly preferred novolac epoxy resins include phenol novolac type epoxy resins because they are easy to handle and have heat resistance.
- the novolac type epoxy resin used in the present embodiment is a known compound, and in this embodiment, a commercially available product can be used.
- the thermal cationic polymerization initiator means a polymerization initiator that generates a cationic species or a Lewis acid by heat, and is represented by the following formula (2).
- Y is BF 4 ⁇ , PF 6 ⁇ , SbF 6 ⁇ , or (BX 4 ) ⁇ (where X is substituted with at least two fluorine or trifluoromethyl groups)
- sulfonium salts for example, triphenylsulfonium boron tetrafluoride, triphenylsulfonium hexafluoride antimony, triphenylsulfonium hexafluoride arsenic, tri (4-methoxyphenyl) sulfonium hexafluoride arsenic, and diphenyl (4- Phenylthiophenyl) sulfonium arsenic hexafluoride and the like.
- Examples of the phosphonium salt include ethyltriphenylphosphonium antimony hexafluoride and tetrabutylphosphonium antimony hexafluoride.
- quaternary ammonium salts include dimethylphenyl (4-methoxybenzyl) ammonium hexafluorophosphate, dimethylphenyl (4-methoxybenzyl) ammonium hexafluoroantimonate, dimethylphenyl (4-methoxybenzyl) ammonium tetrakis ( Pentafluorophenyl) borate, dimethylphenyl (4-methylbenzyl) ammonium hexafluorohexafluorophosphate, dimethylphenyl (4-methylbenzyl) ammonium hexafluoroantimonate, dimethylphenyl (4-methylbenzyl) ammonium hexafluorotetrakis (pentafluoro) Phenyl) borate, methylphenyldibenzylammonium, methylphenyldibenzylammonium hex Fluoroantimonate hexafluorophosphate, methylphenyldi
- the thermal cationic polymerization initiator used in the present embodiment is also a known compound, and a general commercial product can be used in the present embodiment.
- thermal cationic polymerization initiators include, for example, Sun-Aid SI-60, Sun-Aid SI-80, Sun-Aid SI-B3, Sun-Aid SI-B3A and Sun-Aid SI-B4 (all of which are Sanshin Kagaku Kogyo). CXC1612, CXC1738 and CXC1821 (all manufactured by King Industries).
- the novolak type epoxy resin is preferably 90 to 99.5 parts by weight, more preferably 95 to 99.5 parts by weight, and still more preferably 100 parts by weight of the adhesive composition.
- 98 to 99 parts by weight preferably 0.5 to 10 parts by weight, more preferably 0.5 to 5 parts by weight, and still more preferably 1 to 2 parts by weight of a thermal cationic polymerization initiator.
- the novolak type epoxy resin and the thermal cation type polymerization initiator contained in the adhesive composition are within these ranges in that the outgas due to the adhesive composition can be sufficiently reduced.
- the adhesive composition according to this embodiment can be prepared by simply mixing and homogenizing the above two components by a conventional method.
- the adhesive composition may be used as it is, or may optionally be used with an additive component.
- the adhesive composition according to this embodiment is a thermosetting epoxy resin composition excellent in heat resistance, heat cycle resistance and adhesiveness. Moreover, the adhesive composition according to this embodiment contributes to low outgassing.
- the adhesive composition can be used alone or in combination with other additive components, for example, as an adhesive for a gas barrier property evaluation apparatus used in a gas barrier property evaluation apparatus described later.
- Examples of known additive components that can be blended into the adhesive for gas barrier property evaluation apparatus include a curing accelerator, a filler, and a phosphorus compound.
- examples of the curing accelerator include triphenylphosphine, imidazole, aliphatic amine, and thermosetting accelerators such as tertiary and secondary amines.
- examples of the filler include spherical silica, talc, and aluminum oxide. Further, examples of the filler include phosphorus compounds.
- This adhesive for gas barrier property evaluation apparatus may be used with the adhesive composition as it is, or by simply mixing and homogenizing the adhesive composition and the above-described additive components by a conventional method. What is necessary is just to prepare.
- the adhesive layer according to this embodiment contains the above-described adhesive composition.
- the method for forming the adhesive layer is not particularly limited, and first, the adhesive composition may be applied to a substrate or the like, and then, for example, heat treatment may be performed.
- the adhesive layer refers to a state after the adhesive composition is cured by heat treatment or the like.
- the amount of the adhesive composition applied to the base material when forming the adhesive layer is not particularly limited, but is preferably 50 to 200 g / m 2 , more preferably 60 to 150 g / m 2 , and still more preferably. Is 80 to 100 g / m 2 .
- the thickness of the adhesive layer is not particularly limited, but is preferably 38 to 154 ⁇ m, more preferably 46 to 115 ⁇ m, and further preferably 62 to 77 ⁇ m.
- the heating temperature for curing the adhesive composition is not particularly limited, but is preferably 60 to 150 ° C, more preferably 80 to 120 ° C, and further preferably 80 to 100 ° C.
- FIG. 1 is a schematic view schematically showing the configuration of the support bonded body according to the present embodiment.
- the support bonded body 10 includes an adhesive layer 11, a base material 12, and a support body 16.
- the adhesive layer 11 is laminated on the base material 12, and the support 16 is laminated on the adhesive layer 11.
- the support bonded body 10 supports, for example, the film 17.
- a punching metal 15 for preventing deformation of the support 16 is joined to the support joined body 10 by welding to the base 12.
- the support bonded body 10 may be configured not to include the punching metal 15.
- the constituent materials of the substrate 12 and the support 16 and the shape thereof are not particularly limited.
- the substrate 12 is SUS. It is preferable that it is formed from metals, such as.
- the support 16 is preferably formed of a film such as polyimide (PI), polyamide (PA), polyethylene terephthalate (PET), and polyethylene naphthalate (PEN).
- the thickness of the film is not particularly limited, but is preferably 25 to 200 ⁇ m, more preferably 80 to 150 ⁇ m, and further preferably 100 to 125 ⁇ m.
- the support bonded body 10 is obtained, for example, by applying the above-described adhesive composition on the base material 12 and further laminating the support body 16 thereon, and then curing the adhesive composition. It is done.
- FIG. 2 is a schematic diagram schematically showing a configuration of a gas barrier property evaluation apparatus including the support assembly according to the present embodiment. Note that members having the same functions as those already described are denoted by the same reference numerals and description thereof is omitted.
- the gas barrier property evaluation apparatus 20 is an apparatus for measuring moisture permeability such as water vapor of a film or gas permeability such as oxygen, and includes a support assembly 10, a tank 21, and a sample. A chamber 22, a detector 23, and a vacuum pump 24 are provided.
- the support bonded body 10 is provided in the sample chamber 22, and a measurement film 17 is placed on the support bonded body 10.
- Examples of the film 17 used in the gas barrier property evaluation apparatus 20 include an organic EL barrier film and a food film.
- a differential pressure is generated in the sample chamber 22 by the vacuum pump 24. Then, gas is introduced at an arbitrary pressure from the tank 21 side through the film 17, and the vacuum pump 24 side is brought into an ultrahigh vacuum state. Then, moisture or gas flows out of the tank 21 into the sample chamber 22, and the amount of moisture or gas that has passed through the film 17 is detected by the detector 23.
- the adhesive layer 11 included in the support bonded body 10 contains an adhesive composition having excellent heat resistance and thermal cycle characteristics. Therefore, for example, even if the sample chamber 22 is raised to a high temperature of, for example, 80 ° C. to 130 ° C. for the purpose of removing moisture in the sample chamber 22, the heat resistance and thermal cycle characteristics of the adhesive layer 11 are maintained. Also, outgassing can be suppressed. Therefore, the gas barrier property evaluation apparatus 20 can efficiently measure and evaluate the permeability of the film such as moisture or gas.
- the gas barrier property evaluation apparatus of the specific structure shown in FIG. 2 demonstrated the structure provided with the support joined body which concerns on one Embodiment of this invention
- the support joined body which concerns on one Embodiment of this invention is In addition to the gas barrier property evaluation apparatus other than that shown in FIG.
- the gas barrier property evaluation apparatus which can employ the support bonded body according to the embodiment of the present invention is not limited to the one using the differential pressure method and the isobaric method.
- Epoxy resin (phenol novolac type): DIC Corporation, Epicron N-730A Epoxy resin (Bis-A type): ADEKA, Adeka Resin EP-4100 Epoxy resin (PO-added Bis-A type): ADEKA, Adeka Resin EP-4003S Acrylic resin (MMA): manufactured by Tokyo Chemical Industry Co., Ltd., methyl methacrylate epoxy resin (naphthalene paraxylene type): manufactured by Nippon Steel Chemical Co., Ltd., ESPOXY ESN-185 Epoxy resin (multifunctional type): Tetraglycidyldiaminodiphenylmethane (YH-434) manufactured by Tohto Kasei Co., Ltd.
- Epoxy resin (hydrogenated Bis-A type): manufactured by Yuka Shell Epoxy, Epicoat 828EL Thermal cationic polymerization initiator: SI-60L, manufactured by Sanshin Chemical Co., Ltd.
- Photocationic polymerization initiator Adeka Arcles SP-170, manufactured by ADEKA Curing agent (naphthalene paraxylene novolac resin): manufactured by Nippon Steel Chemical Co., Ltd., SN-180 Curing agent (phenol novolac resin): Sumitrite Resin PR-53195, manufactured by Sumitomo Durres Curing accelerator (triphenylphosphine): manufactured by Wako Pure Chemical Industries, Ltd., primary filler (spherical silica): manufactured by Denka Co., Ltd., FB-6S Phosphorus compound (9,10-dihydro-9-oxa-10-phosphaphenanthrene-10-oxide): SANKO-HCA, manufactured by Sanko Chemical Co., Ltd.
- test piece Using a doctor blade YD-3 manufactured by Yoshimitsu Seiki Co., Ltd., a coating film having a thickness of 100 ⁇ m is formed by applying each adhesive composition to Examples 1 to 3 and Comparative Examples 1 to 9 on a substrate. did. Then, film-shaped test pieces were obtained by performing the following treatments on Examples 1 to 3, Comparative Examples 1 and 2, and Comparative Examples 3 to 5.
- Examples 1 to 3 and Comparative Examples 1 and 2 Thermosetting epoxy resin adhesive
- the base material on which the coating film was formed was subjected to a heat treatment at 100 ° C. for 2 hours to cure the coating film to obtain a film-like test piece.
- Test Example 1 The test shown below was done about each of the obtained test piece.
- Outgas measurement 1 g of each of the test pieces of Examples 1 to 3 and Comparative Examples 1 to 9 described above was collected in a vial and heated in a headspace at 85 ° C. for 30 minutes in a gas chromatography Clarus 500 manufactured by Birkin Elmer. The amount of outgas was measured. The outgas amount was calculated from the total area amount of each test piece on the basis of the detection area of the test piece having a known outgas amount.
- ⁇ Heat cycle resistance> The obtained support joined body was heated at 40 ° C. for 1 hour in a constant temperature bath DNE601 manufactured by Yamato Scientific Co., Ltd., then heated from 40 ° C. to 150 ° C. at a heating rate of 1 ° C./min. A cycle was used, and it was confirmed whether changes (wrinkles, peeling, etc.) occurred in the appearance of the sample every time one cycle was completed.
- the adhesive composition of each example has good heat resistance, adhesiveness, and heat cycle resistance, and contributes to low outgassing. Furthermore, when judged comprehensively, it was recognized that the adhesive composition of Example 1 was the most excellent.
- the adhesive composition of the present invention can be used as an adhesive suitably used also in a gas barrier property evaluation apparatus.
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Abstract
Description
本実施形態に係る接着剤組成物(以下、単に「接着剤組成物」ともいう)は、ノボラック型エポキシ樹脂と、熱カチオン型重合開始剤とを含有するものである。
本実施形態に係る接着剤層は、上記した接着剤組成物を含有するものである。この接着剤層を形成する方法は特に限定されず、まず接着剤組成物を基材等に塗布し、その後、例えば加熱処理を行えばよい。なお、本明細書において接着剤層は、接着剤組成物が加熱処理等によって硬化した後の状態を指すものとする。
図1は、本実施形態に係る支持接合体の構成を概略的に示す模式図である。図1を参照して説明すると、支持接合体10は、接着剤層11と、基材12と、支持体16とを備えている。接着剤層11は基材12に積層されており、支持体16は接着剤層11に積層されている。この支持接合体10は、例えばフィルム17を支持するものである。
図2は、本実施形態に係る支持接合体を備えたガスバリア性評価装置の構成を概略的に示す模式図である。なお、既に説明した部材と同一の機能を有する部材については同一符号を付し、その説明を省略する。
(1)接着剤組成物の調製:
表1に示す各成分を混合して、実施例1~3および比較例1~9の接着剤組成物を調製した。なお、各成分の配合量を示す数値の単位は重量部である。また、各成分の詳細は以下の通りである。
エポキシ樹脂(フェノールノボラック型):DIC社製、エピクロンN-730A
エポキシ樹脂(Bis-A型):ADEKA社製、アデカレジンEP-4100
エポキシ樹脂(PO付加型Bis-A型):ADEKA社製、アデカレジンEP-4003S
アクリル樹脂(MMA):東京化成工業社製、メタクリル酸メチル
エポキシ樹脂(ナフタレンパラキシレン型):新日鐵化学社製、エスポキシESN-185
エポキシ樹脂(多官能性型):東都化成社製、テトラグリシジルジアミノジフェニルメタン(YH-434)
エポキシ樹脂(水素化Bis-A型):油化シェルエポキシ社製、エピコート828EL
熱カチオン型重合開始剤:三新化学社製、SI-60L
光カチオン型重合開始剤:ADEKA社製、アデカアークルズSP-170
硬化剤(ナフタレンパラキシレンノボラック樹脂):新日鐵化学社製、SN-180
硬化剤(フェノールノボラック樹脂):住友デュレス社製、スミライトレジンPR-53195
硬化促進剤(トリフェニルホスフィン):和光純薬工業社製、一級
充填剤(球状シリカ):デンカ株式会社製、FB-6S
リン化合物(9,10-ジヒドロ-9-オキサ-10-フォスファフェナントレン-10‐オキサイド):三光化学社製、SANKO-HCA
(2)試験片の作製:
ヨシミツ精機社製ドクターブレードYD-3型を用いて、実施例1~3および比較例1~9について、それぞれの接着剤組成物を基材に塗布することで、厚さ100μmの塗膜を成形した。それから、実施例1~3および比較例1,2と、比較例3~5に対しては次の処理を行うことで、フィルム状の試験片を得た。
塗膜を成形した基材に100℃で2時間加熱処理を行って塗膜を硬化して、フィルム状の試験片を得た。
塗膜を成形した基材に、ウシオ電機社製メタルハライドランプUVC-1212を用いて6000mJ/cm2(365nm)を照射して、80℃で1時間加熱することによって塗膜を硬化して、フィルム状の試験片を得た。
得られた試験片のそれぞれについて、以下に示す試験を行った。
(a)耐熱性の測定:
ブルカー社製示差走査熱量計DSC7000Sを用いて、昇温速度10℃/minで加熱した際のDSCサーモグラムの変曲点を測定し、この変曲点をガラス転移温度とした。
ガラス転移温度が150℃以上であれば耐熱性に「優れる:◎」、ガラス転移温度が149℃~130℃であれば耐熱性が「良好:○」、ガラス転移温度が130℃未満であれば耐熱性に「劣る:×」とし、評価結果とした。結果を表1に示す。
(a)アウトガスの測定:
上記した実施例1~3および比較例1~9の各試験片1gをバイアル瓶に採取し、バーキンエルマー社製ガスクロマトグラフィーClarus500にて、ヘッドスペース内で85℃、30分間加温した後、アウトガス量を測定した。アウトガス量は、アウトガス量の既知の試験片の検出面積を基準に、各試験片の総面積量より算出した。
アウトガス量が100ppm以下であればアウトガス量の低減効果に「優れる:◎」、101ppm~500ppm以下であればアウトガス量の低減効果が「良好:○」、500ppm超であればアウトガス量の低減効果に「劣る:×」とし、評価結果とした。結果を表1に示す。
(1)接着剤組成物の調製:
上記した製造例1と同様にして、実施例1~3および比較例1~9の接着剤組成物を調製した。
それぞれの接着剤組成物を用いて基材(SUS306製)と支持体としてのフィルム(東レ・デュポン社製、厚さ125μm、ポリイミド)との接着面積が1cm2になるようにして貼り合わせ、支持接合体を形成した。
得られた支持接合体について、以下に示す試験を行った。
(a)破壊状態の観察:
支持接合体に対して、島津製作所製オートグラフAGH-Hを用いて、25℃環境下、引張速度5mm/minでせん断方向に応力をかけ、その際の破壊状態を観察した。
支持体としてのフィルムが破壊すれば、接着性が「優れる:◎」、支持体としてのフィルムが凝集し破壊すれば、接着性が「良好:○」、支持体としてのフィルムまたは基材から界面剥離が生じれば、接着性が「悪い:×」とし、評価結果とした。結果を表1に示す。
得られた支持接合体を、ヤマト科学社製恒温槽DNE601にて40℃1時間加熱し、次に40℃から150℃まで昇温速度1℃/minで昇温させ、150℃1時間を1サイクルとし、1サイクル終わる毎にサンプルの外観に変化(しわおよびはがれ等)が生じていないかを確認した。
サンプルの外観に変化が生じたのが、10サイクル以上であれば熱サイクル耐性が「優れる:◎」、2~9サイクルであれば熱サイクル耐性が「良好:○」、1サイクル以下であれば熱サイクル耐性が「悪い:×」とし、評価結果とした。結果を表1に示す。
11・・・接着剤層
12・・・基材
16・・・支持体
17・・・フィルム
18・・・保持部
20・・・ガスバリア性評価装置
21・・・タンク
22・・・試料チャンバー
24・・・真空ポンプ
Claims (7)
- 前記ノボラック型エポキシ樹脂として、フェノールノボラック型エポキシ樹脂、キシレンノボラック型エポキシ樹脂、ジシクロペンタジエン(DCPD)フェノールノボラック型エポキシ樹脂およびビフェニルノボラック型エポキシ樹脂からなる群から選択される1種または2種以上を含有することを特徴とする請求項1に記載の接着剤組成物。
- 前記ノボラック型エポキシ樹脂90~99.5重量部と、前記熱カチオン型重合開始剤10~0.5重量部とを含有することを特徴とする請求項1または2に記載の接着剤組成物。
- 請求項1~3のいずれか1項に記載の接着剤組成物を含有することを特徴とするガスバリア性評価装置用接着剤。
- 請求項1~3のいずれか1項に記載の接着剤組成物を含有することを特徴とする接着剤層。
- 基材と、
前記基材に積層された接着剤層と、
前記接着剤層に積層された支持体とを備えた支持接合体であって、
前記接着剤層は、請求項5に記載された接着剤層であることを特徴とする支持接合体。 - 請求項6に記載の支持接合体を備えることを特徴とするガスバリア性評価装置。
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CN201780055698.9A CN109804034B (zh) | 2016-10-07 | 2017-08-24 | 粘合剂组合物及含其的粘合剂层、支撑接合体,及具备该支撑接合体的阻气性评价装置 |
KR1020197006368A KR102195770B1 (ko) | 2016-10-07 | 2017-08-24 | 접착제 조성물 및 이를 함유하는 접착제층, 지지 접합체 및 이 지지 접합체를 구비하는 가스 배리어성 평가 장치 |
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TW201816056A (zh) | 2018-05-01 |
CN109804034B (zh) | 2021-12-10 |
KR20190034326A (ko) | 2019-04-01 |
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CN109804034A (zh) | 2019-05-24 |
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